CN109911228A - A kind of unmanned plane shrinking protection automatically with exploration camera - Google Patents
A kind of unmanned plane shrinking protection automatically with exploration camera Download PDFInfo
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- CN109911228A CN109911228A CN201910154028.3A CN201910154028A CN109911228A CN 109911228 A CN109911228 A CN 109911228A CN 201910154028 A CN201910154028 A CN 201910154028A CN 109911228 A CN109911228 A CN 109911228A
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Abstract
The present invention provides a kind of unmanned plane for shrinking protection automatically with exploration camera, its structure includes unmanned plane main body, shaft, the unmanned plane during flying wing, shaft attachment base, camera protection device, it is connected above camera protection device with below unmanned plane main body, the unmanned plane during flying wing is fixedly installed in shaft upper end, shaft and shaft attachment base are mechanically connected, shaft attachment base is fixedly installed in unmanned plane main body, the quantity of the unmanned plane during flying wing is four, energization trigger mechanism contacts ground first and triggers energization so that the electromagnet triggering on protection mechanism is powered and adsorbs camera contracting mechanism upwards by self gravity during unmanned plane falls, so that the camera in camera contracting mechanism is retracted to inside shrink cylinder first, then camera contracting mechanism is adsorbed to inside protection mechanism, prevent camera rough It is bumped to and damages by rubble on mountainous region.
Description
Technical field
The present invention is a kind of unmanned plane for shrinking protection automatically with exploration camera, belongs to air vehicle technique field.
Background technique
Unmanned plane is used often in geological environment exploration and carries out camera shooting exploration, when in the process surveyed to mountainous region
In, mountainous region ground relief and there are more rubble, when unmanned plane, which lands, to stop, unmanned plane exploration camera often can
It is affected.
Based on foregoing description the inventors discovered that, it is existing a kind of to shrink the unmanned plane of protection automatically with exploration camera
There is night maintenance the electric power box of mosquito expulsion function to be primarily present following deficiency, such as:
Due to exploration mountain environment ground relief and rubble is more, so that exploration unmanned plane is after landing due to exploration
Camera collides rubble often, camera is caused to damage outside being exposed to.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides it is a kind of with exploration camera shrink automatically protection nobody
Machine solves due to exploration mountain environment ground relief and rubble is more, so that exploration unmanned plane is after landing due to surveying
Outside survey camera is exposed to, the problem of colliding rubble often, camera caused to damage.
(2) technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs: one kind has exploration camera automatic
The unmanned plane of protection is shunk, structure includes unmanned plane main body, shaft, the unmanned plane during flying wing, shaft attachment base, camera head protecting
Device, the camera protection device top and unmanned plane main body lower section are connected, and the unmanned plane during flying wing is fixedly installed in
Shaft upper end, the shaft and shaft attachment base are mechanically connected, and the shaft attachment base is fixedly installed in unmanned plane main body, institute
State the unmanned plane during flying wing quantity be four, the unmanned plane main body be it is horizontal positioned, the unmanned plane during flying wing set on nobody
Above owner's body, the camera protection device includes support leg, the first conducting wire, energization trigger mechanism, the second conducting wire, protection machine
Structure, battery, first interface, second interface, the energization trigger mechanism are mutually welded with support leg, the first conducting wire right end with
It is connected on the left of energization trigger mechanism, second conducting wire upper end, which is connected to the battery, to be connect, and the first interface is set to second and connects
On the right side of mouthful, the protection mechanism is set to above energization trigger mechanism, and first conducting wire upper end is connected with second interface, described
First interface is integrated with protection mechanism, and the first interface, which is connected to the battery, to be connect, and the protection mechanism is installed on
Below unmanned plane main body, the support leg is welded in below unmanned plane main body.
Preferably, the energization trigger mechanism include triggering chamber, compressed spring, right contact block, right feeler lever, compression bar, left feeler lever,
Left contact block, the compressed spring are installed between the intracavitary upper side of triggering and compression bar upper end, and the right contact block is set on right feeler lever
Side, the right contact block are fixedly installed on triggering chamber, and the right feeler lever left end is welded in compression bar side, and the left feeler lever is set to a left side
Below contact block, the left feeler lever right end is welded in compression bar side, and the left contact block is fixedly installed on triggering chamber, the triggering chamber
Be it is horizontal positioned, fit on the outside of the compression bar with triggering chamber through-hole inside, the triggering chamber is mutually welded with support leg, the pressure
Contracting spring has the elastic force being pressed downward.
Preferably, the protection mechanism includes left connecting line, electromagnet, right connecting line, auxiliary mobile mechanism, camera receipts
Contracting mechanism, reset spring, exocoel, mounting blocks, the left connecting line right end are connected with electromagnet, and the right connecting line is set to a left side
On the right side of connecting line, the right connecting line left end is connected with electromagnet, and the electromagnet upper end is fixedly installed on exocoel inside
Side, the auxiliary mobile mechanism are connected with camera contracting mechanism, the camera contracting mechanism outside and phase on the inside of exocoel
Fitting, the reset spring upper end are welded on the downside of mounting blocks, and the quantity of the reset spring is two, the mounting blocks left end
It is welded on exocoel, the electromagnet is set to above camera contracting mechanism, and the quantity of the auxiliary mobile mechanism is two, institute
It states and is installed on the upside of exocoel below unmanned plane main body, the electromagnet has the magnetic force for adsorbing camera contracting mechanism upwards,
The reset spring has downward elastic force, and the auxiliary mobile mechanism can assist stablizing movement.
Preferably, the auxiliary mobile mechanism includes sliding rail, nut, connecting rod, bolt, on the left of the sliding rail and connecting rod
Right side fits, and the nut inner thread is threadedly coupled with bolt external screw thread, fits on the right side of the sliding rail with nut left side, institute
Nut is stated on the right side of connecting rod, the connecting rod is mutually welded with camera contracting mechanism, and the sliding rail is fixedly installed in exocoel
On, the nut is used cooperatively with bolt has the function of fixation.
Preferably, the camera contracting mechanism includes shrink cylinder, through-hole, absorption iron plate, camera, thrust spring, leads
Way roller drags messenger, and the shrink cylinder is integrated with through-hole, and the through-hole is set to above absorption iron plate, the absorption
It fits on the outside of iron plate with shrink cylinder inside, the absorption iron plate lower end is connected with messenger upper end is dragged, on the outside of the camera
It fits on the inside of shrink cylinder lower-side hole, the thrust spring is installed on the right side of camera and on the inside of shrink cylinder between the left side, institute
It states guide roller to be fixedly installed in shrink cylinder, described drag is connected on the right side of messenger lower end and camera, described to drag on the outside of messenger
It fits with guide roller inside, is mutually welded on the outside of the shrink cylinder with connecting rod, the work dragged messenger and there is tethered sliding
With the thrust spring has elastic force to the left.
(3)Beneficial effect
When unmanned plane, which surveys, to land, compression bar contacts ground first, so that compressed spring is compressed, the right feeler lever of compression bar two sides
Right contact block and left contact block are contacted respectively with left feeler lever, so that electromagnet is powered, the absorption iron plate of electromagnet absorption lower section, so that inhaling
Attached iron plate moves up along shrink cylinder, adsorbs iron plate by dragging messenger and camera is drawn in the right shrink cylinder around guide roller
Inside when absorption iron plate, which is moved to above shrink cylinder, to be locked, while driving in shrink cylinder phase along through-hole below exocoel
Mobile, so that shrink cylinder is retracted to outer chamber, reset spring is compressive state at this time, so that camera is from extraneous shadow
It rings, wherein connecting rod slides up and down moving for stabilized contraction cylinder along sliding rail, prevents from deviating；After unmanned plane during flying gets up, pressure
Bar makes compressed spring elasticity restore to push compression bar due to lose own wt, so that circuit disconnects, electromagnet power-off is received
Contracting cylinder moves down stretching by reset spring elastic restoring force, during this reset spring also by thrust spring elasticity
Restoring force fails to agree pop-up.
When unmanned plane fall during energization trigger mechanism contact first ground by self gravity triggering energization so that
Electromagnet triggering on protection mechanism is powered adsorbs camera contracting mechanism upwards, so that the camera shooting in camera contracting mechanism
Head is retracted to inside shrink cylinder first, and then camera contracting mechanism is adsorbed to inside protection mechanism, prevents camera recessed
It is bumped to and damaged by rubble on the mountainous region of convex injustice.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram for the unmanned plane for shrinking protection automatically with exploration camera of the present invention；
Fig. 2 is the structural schematic diagram of the right view of camera protection device of the present invention；
Fig. 3 is the structural schematic diagram of energization trigger mechanism of the present invention；
Fig. 4 is the structural schematic diagram of camera contracting mechanism left view of the present invention；
Fig. 5 is the structural schematic diagram of the present invention auxiliary right view of mobile mechanism；
Fig. 6 is the structural schematic diagram of the right view of camera contracting mechanism of the present invention.
In figure: unmanned plane main body -1, shaft -2, the unmanned plane during flying wing -3, shaft attachment base -4, camera protection device -
5, support leg -51, the first conducting wire -52, energization trigger mechanism -53, the second conducting wire -54, camera contracting mechanism -55, battery -
56, first interface -57, second interface -58, triggering chamber -531, compressed spring -532, right contact block -533, right feeler lever -534, pressure
Bar -535, left feeler lever -536, left contact block -537, left connecting line -551, electromagnet -552, right connecting line -553, auxiliary moving machine
Structure -554, camera contracting mechanism -555, reset spring -556, exocoel -557, mounting blocks -558, sliding rail -5541, nut -
5542, connecting rod -5543, bolt -5544, shrink cylinder -5551, through-hole -5552, absorption iron plate -5553, camera -5554, push away
Power spring -5555, drags messenger -5557 at guide roller -5556.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As shown in figures 1 to 6, the embodiment of the present invention provides a kind of unmanned plane for shrinking protection automatically with exploration camera,
Structure includes unmanned plane main body 1, shaft 2, the unmanned plane during flying wing 3, shaft attachment base 4, camera protection device 5, the camera shooting
The top of head protection device 5 be connected below unmanned plane main body 1, the unmanned plane during flying wing 3 is fixedly installed in 2 upper end of shaft,
The shaft 2 is mechanically connected with shaft attachment base 4, and the shaft attachment base 4 is fixedly installed in unmanned plane main body 1, the nothing
The quantity of man-machine flying wing 3 is four, the unmanned plane main body 1 be it is horizontal positioned, the unmanned plane during flying wing 3 is set on unmanned plane
1 top of main body, the camera protection device 5 include support leg 51, the first conducting wire 52, energization trigger mechanism 53, the second conducting wire
54, protection mechanism 55, battery 56, first interface 57, second interface 58, the energization trigger mechanism 53 are welded with 51 phase of support leg
It connects, is connected on the left of 52 right end of the first conducting wire and energization trigger mechanism 53,54 upper end of the second conducting wire and battery 56
It is connected, the first interface 57 is set to 58 right side of second interface, and the protection mechanism 55 is set to 53 top of energization trigger mechanism,
First conducting wire, 52 upper end is connected with second interface 58, and the first interface 57 is integrated with protection mechanism 55,
The first interface 57 is connected with battery 56, and the protection mechanism 55 is installed on 1 lower section of unmanned plane main body, the support leg
51 are welded in 1 lower section of unmanned plane main body.
The energization trigger mechanism 53 includes triggering chamber 531, compressed spring 532, right contact block 533, right feeler lever 534, compression bar
535, left feeler lever 536, left contact block 537, the compressed spring 532 be installed on triggering 531 inside front of chamber and 535 upper end of compression bar it
Between, the right contact block 533 is set to right 534 top of feeler lever, and the right contact block 533 is fixedly installed on triggering chamber 531, the right touching
534 left end of bar is welded in 535 side of compression bar, and the left feeler lever 536 is set to left 537 lower section of contact block, left 536 right end of the feeler lever weldering
It is connected to 535 side of compression bar, the left contact block 537 is fixedly installed on triggering chamber 531, and the triggering chamber 531 is horizontal positioned, institute
It states and fits on the inside of 535 outside of compression bar and triggering 531 through-hole of chamber, the triggering chamber 531 is welded with 51 phase of support leg, the compression
Spring 532 has the elastic force for being pressed downward compression bar 535.
The protection mechanism 55 include left connecting line 551, electromagnet 552, right connecting line 553, auxiliary mobile mechanism 554,
Camera contracting mechanism 555, reset spring 556, exocoel 557, mounting blocks 558, left 551 right end of connecting line and electromagnet
552 are connected, and the right connecting line 553 is set to left 551 right side of connecting line, right 553 left end of connecting line and 552 phase of electromagnet
Connection, 552 upper end of electromagnet are fixedly installed in 557 inside front of exocoel, and the auxiliary mobile mechanism 554 receives with camera
Contracting mechanism 555 is connected, 555 outside of the camera contracting mechanism with fit on the inside of exocoel 557, the reset spring 556
Upper end is welded in 558 downside of mounting blocks, and the quantity of the reset spring 556 is two, and 558 left end of mounting blocks is welded in outer
On chamber 557, the electromagnet 552 is set to 555 top of camera contracting mechanism, and the quantity of the auxiliary mobile mechanism 554 is two
It is a, 1 lower section of unmanned plane main body is installed on the upside of the exocoel 557, the electromagnet 552 has camera contracting mechanism 555
The magnetic force adsorbed upwards, the reset spring 556 have the elastic force for resetting camera contracting mechanism 555 downwards, and the auxiliary is moved
Motivation structure 554 being capable of the stable movement of about 555 auxiliary camera contracting mechanism.
The auxiliary mobile mechanism 554 includes sliding rail 5541, nut 5542, connecting rod 5543, bolt 5544, the sliding rail
5541 left side with fit on the right side of connecting rod 5543,5542 internal screw thread of nut is threadedly coupled with 5544 external screw thread of bolt, institute
It states 5541 right side of sliding rail and fits on the left of nut 5542, the nut 5542 is set to 5543 right side of connecting rod, the connecting rod
5543 weld with 555 phase of camera contracting mechanism, and the sliding rail 5541 is fixedly installed on exocoel 557, the nut 5542 with
Bolt 5544, which is used cooperatively, to be had the function of for connecting rod 5543 being bonded with the fixation of sliding rail 5541.
The camera contracting mechanism 555 include shrink cylinder 5551, through-hole 5552, absorption iron plate 5553, camera 5554,
Thrust spring 5555, guide roller 5556 drag messenger 5557, and the shrink cylinder 5551 is integrated with through-hole 5552, institute
State through-hole 5552 and be set to absorption iron plate 5553 top, on the outside of the absorption iron plate 5553 with fit on the inside of shrink cylinder 5551, institute
It states absorption 5553 lower end of iron plate to be connected with 5557 upper end of messenger is dragged, 5554 outside of camera and 5551 lower-side hole of shrink cylinder
Inside fits, and the thrust spring 5555 is installed between 5554 right side of camera and the 5551 inside left side of shrink cylinder, described
Guide roller 5556 is fixedly installed in shrink cylinder 5551, and described drag is connected on the right side of 5557 lower end of messenger and camera 5554,
Described to drag 5557 outside of messenger and fit on the inside of guide roller 5556,5551 outside of the shrink cylinder is welded with 5543 phase of connecting rod
It connects, the messenger 5557 of dragging has the function of that drawing camera 5554 moves right, and the thrust spring 5555 has to be pushed away to the left
The elastic force of dynamic camera 5554.
Working principle: when unmanned plane, which surveys, to land, compression bar 535 contacts ground first, so that compressed spring 532 is compressed,
The right feeler lever 534 of 535 two sides of compression bar contacts right contact block 533 and left contact block 537 with left feeler lever 536 respectively, so that electromagnet 552 is logical
The absorption iron plate 5553 of electricity, the absorption of electromagnet 552 lower section is inhaled so that absorption iron plate 5553 moves up along shrink cylinder 5551
Attached iron plate 5553 is drawn in the right camera 5554 inside shrink cylinder 5551 around guide roller 5556 by dragging messenger 5557, when
Absorption iron plate 5553 is moved to above shrink cylinder 5551 when being locked, while driving in 5551 phase of shrink cylinder along exocoel 557
Lower section through-hole is mobile, so that shrink cylinder 5551 is retracted to inside exocoel 557, reset spring 556 is compressive state at this time, so that
Camera 5554 is from external influence, and wherein connecting rod 5543 slides up and down the shifting of stabilized contraction cylinder 5551 along sliding rail 5541
It is dynamic, it prevents from deviating；After unmanned plane during flying gets up, compression bar 535 due to lose own wt make compressed spring 532 elasticity it is extensive
Multiple to push compression bar 535, so that circuit disconnects, electromagnet 552 is powered off, and shrink cylinder 5551 is restored by 556 elasticity of reset spring
Power moves down stretching, and reset spring 556 fails to agree pop-up also by the elastic restoring force of thrust spring 5555 during this.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. a kind of shrink the unmanned plane of protection with exploration camera automatically, structure include unmanned plane main body (1), shaft (2),
The unmanned plane during flying wing (3), shaft attachment base (4), camera protection device (5), it is characterised in that:
It is connected above the camera protection device (5) with unmanned plane main body (1) lower section, the unmanned plane during flying wing (3) is solid
Dingan County is loaded on shaft (2) upper end, and the shaft (2) and shaft attachment base (4) are mechanically connected, and the shaft attachment base (4) is fixed
It is installed on unmanned plane main body (1), the quantity of the unmanned plane during flying wing (3) is four, and the unmanned plane main body (1) is level
It places, the unmanned plane during flying wing (3) is set to above unmanned plane main body (1)；
The camera protection device (5) includes support leg (51), the first conducting wire (52), energization trigger mechanism (53), second leads
Line (54), protection mechanism (55), battery (56), first interface (57), second interface (58), the energization trigger mechanism (53)
It mutually welds with support leg (51), is connected on the left of the first conducting wire (52) right end and energization trigger mechanism (53), described second
Conducting wire (54) upper end is connected with battery (56), and the first interface (57) is set on the right side of second interface (58), the protection
Mechanism (55) is set to above energization trigger mechanism (53), and the first conducting wire (52) upper end is connected with second interface (58), institute
First interface (57) to be stated to be integrated with protection mechanism (55), the first interface (57) is connected with battery (56),
The protection mechanism (55) is installed below unmanned plane main body (1), and the support leg (51) is welded under unmanned plane main body (1)
Side.
2. a kind of unmanned plane for shrinking protection automatically with exploration camera according to claim 1, it is characterised in that: institute
Stating energization trigger mechanism (53) includes triggering chamber (531), compressed spring (532), right contact block (533), right feeler lever (534), compression bar
(535), left feeler lever (536), left contact block (537), the compressed spring (532) are installed on triggering chamber (531) inside front and pressure
Between bar (535) upper end, the right contact block (533) is set to above right feeler lever (534), and the right contact block (533) is fixedly installed in
It triggers on chamber (531), right feeler lever (534) left end is welded in compression bar (535) side, and the left feeler lever (536) is set to left touching
Below block (537), left feeler lever (536) right end is welded in compression bar (535) side, and the left contact block (537) is fixedly installed in
Trigger on chamber (531), the triggering chamber (531) be it is horizontal positioned, the compression bar (535) outside and trigger in chamber (531) through-hole
Side fits, and the triggering chamber (531) is mutually welded with support leg (51).
3. a kind of unmanned plane for shrinking protection automatically with exploration camera according to claim 1, it is characterised in that: institute
State protection mechanism (55) include left connecting line (551), electromagnet (552), right connecting line (553), auxiliary mobile mechanism (554),
Camera contracting mechanism (555), reset spring (556), exocoel (557), mounting blocks (558), left connecting line (551) right end
It is connected with electromagnet (552), the right connecting line (553) is set on the right side of left connecting line (551), the right connecting line (553)
Left end is connected with electromagnet (552), and electromagnet (552) upper end is fixedly installed in exocoel (557) inside front, described auxiliary
Mobile mechanism (554) is helped to be connected with camera contracting mechanism (555), camera contracting mechanism (555) outside and exocoel
(557) inside fits, and reset spring (556) upper end is welded on the downside of mounting blocks (558), the reset spring (556)
Quantity be two, mounting blocks (558) left end is welded on exocoel (557), the electromagnet (552) be set to camera receipts
Above contracting mechanism (555), the quantity of auxiliary mobile mechanism (554) is two, is installed on nobody on the upside of the exocoel (557)
Below owner's body (1).
4. a kind of unmanned plane for shrinking protection automatically with exploration camera according to claim 3, it is characterised in that: institute
Stating auxiliary mobile mechanism (554) includes sliding rail (5541), nut (5542), connecting rod (5543), bolt (5544), the sliding rail
(5541) it fits on the right side of left side and connecting rod (5543), nut (5542) internal screw thread and bolt (5544) external screw thread screw thread
Connection, sliding rail (5541) right side and nut (5542) left side fit, and the nut (5542) is set to connecting rod (5543)
Right side, the connecting rod (5543) are mutually welded with camera contracting mechanism (555), and the sliding rail (5541) is fixedly installed in exocoel
(557) on.
5. a kind of unmanned plane for shrinking protection automatically with exploration camera according to claim 3 or 4, feature exist
In: the camera contracting mechanism (555) includes shrink cylinder (5551), through-hole (5552), absorption iron plate (5553), camera
(5554), thrust spring (5555), guide roller (5556), drag messenger (5557), the shrink cylinder (5551) and through-hole
(5552) it is integrated, the through-hole (5552) is set to above absorption iron plate (5553), and the absorption iron plate (5553) is outside
It fits on the inside of side and shrink cylinder (5551), the absorption iron plate (5553) lower end is connected with messenger (5557) upper end is dragged, institute
It states and fits on the outside of camera (5554) with shrink cylinder (5551) lower-side hole inside, the thrust spring (5555) is installed on camera shooting
On the right side of head (5554) between the left side of shrink cylinder (5551) inside, the guide roller (5556) is fixedly installed in shrink cylinder
(5551) on, described drag is connected on the right side of messenger (5557) lower end and camera (5554), it is described drag on the outside of messenger (5557) with
It fits on the inside of guide roller (5556), is mutually welded on the outside of the shrink cylinder (5551) with connecting rod (5543).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910154028.3A CN109911228A (en) | 2019-03-01 | 2019-03-01 | A kind of unmanned plane shrinking protection automatically with exploration camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910154028.3A CN109911228A (en) | 2019-03-01 | 2019-03-01 | A kind of unmanned plane shrinking protection automatically with exploration camera |
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| Publication Number | Publication Date |
|---|---|
| CN109911228A true CN109911228A (en) | 2019-06-21 |
Family
ID=66962931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910154028.3A Pending CN109911228A (en) | 2019-03-01 | 2019-03-01 | A kind of unmanned plane shrinking protection automatically with exploration camera |
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| Country | Link |
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| CN (1) | CN109911228A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110766904A (en) * | 2019-11-04 | 2020-02-07 | 苏州力佳达电子科技有限公司 | Monitoring device who contains smoke transducer and shower nozzle |
| CN112238950A (en) * | 2020-11-06 | 2021-01-19 | 吉林大学 | Fixed wing remote sensing unmanned aerial vehicle with spectrum camera protection device |
| CN112478161A (en) * | 2020-12-12 | 2021-03-12 | 安徽普华灵动机器人科技有限公司 | Unmanned aerial vehicle for electric power inspection |
| CN116039983A (en) * | 2023-01-11 | 2023-05-02 | 江苏航运职业技术学院 | Unmanned aerial vehicle with photogrammetry function |
-
2019
- 2019-03-01 CN CN201910154028.3A patent/CN109911228A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110766904A (en) * | 2019-11-04 | 2020-02-07 | 苏州力佳达电子科技有限公司 | Monitoring device who contains smoke transducer and shower nozzle |
| CN112238950A (en) * | 2020-11-06 | 2021-01-19 | 吉林大学 | Fixed wing remote sensing unmanned aerial vehicle with spectrum camera protection device |
| CN112238950B (en) * | 2020-11-06 | 2022-07-26 | 吉林大学 | Fixed wing remote sensing unmanned aerial vehicle with spectrum camera protection device |
| CN112478161A (en) * | 2020-12-12 | 2021-03-12 | 安徽普华灵动机器人科技有限公司 | Unmanned aerial vehicle for electric power inspection |
| CN116039983A (en) * | 2023-01-11 | 2023-05-02 | 江苏航运职业技术学院 | Unmanned aerial vehicle with photogrammetry function |
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